CN1807847A - Turbocharger - Google Patents

Turbocharger Download PDF

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Publication number
CN1807847A
CN1807847A CNA2005101317221A CN200510131722A CN1807847A CN 1807847 A CN1807847 A CN 1807847A CN A2005101317221 A CNA2005101317221 A CN A2005101317221A CN 200510131722 A CN200510131722 A CN 200510131722A CN 1807847 A CN1807847 A CN 1807847A
Authority
CN
China
Prior art keywords
material layer
turbosupercharger
woodruff key
turbine
described turbosupercharger
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CNA2005101317221A
Other languages
Chinese (zh)
Other versions
CN1807847B (en
Inventor
D·弗兰肯施泰因
R·贝宁
H·韦斯
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BorgWarner Inc
Original Assignee
BorgWarner Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by BorgWarner Inc filed Critical BorgWarner Inc
Publication of CN1807847A publication Critical patent/CN1807847A/en
Application granted granted Critical
Publication of CN1807847B publication Critical patent/CN1807847B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12Control of the pumps
    • F02B37/24Control of the pumps by using pumps or turbines with adjustable guide vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00Regulating or controlling by varying flow
    • F01D17/10Final actuators
    • F01D17/12Final actuators arranged in stator parts
    • F01D17/14Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12Control of the pumps
    • F02B37/22Control of the pumps by varying cross-section of exhaust passages or air passages, e.g. by throttling turbine inlets or outlets or by varying effective number of guide conduits
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/40Application in turbochargers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/70Slinger plates or washers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/70Shape
    • F05D2250/71Shape curved
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/20Heat transfer, e.g. cooling
    • F05D2260/231Preventing heat transfer
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/30Retaining components in desired mutual position

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Supercharger (AREA)

Abstract

The present invention provides a turbocharger comprising a cartridge which is arranged in a turbine casing for variable turbine geometry; a bearing housing which is arranged between the turbine casing and a compressor housing of a compressor impeller and in which a bearing assembly is arranged for a shaft which supports the turbine wheel and the compressor impeller; and a woodruff key which is arranged between the cartridge and the bearing housing, the woodruff key being composed of at least two material layers.

Description

Turbosupercharger
Invention field
The present invention relates to a kind of turbosupercharger.
This turbosupercharger can be known from WO 2004/048755 A.
Background technique
Another kind of turbosupercharger is known from EP 1398463A1.In turbo-side, in described turbosupercharger, heat shield plate is set around its axle.This heat shield plate is used to protect the bearing housing can be by owing to do not flow through the damage that high temperature that the waste gas of the internal-combustion engine of this turbine produces causes.This known heat shield plate is made of the part of single one deck, yet the thermal insulating properties of this part needs to improve.
EP 0160460B1 has announced another kind of assembly.This assembly uses at a woodruff key wanting to produce on the supporting blades annulus of axial restraint an axial dipole field power.Since far away from turbine wheel, therefore, on described position, do not need adiabatic function.
Summary of the invention
Therefore, the objective of the invention is to provide the turbosupercharger of form described in the preface of claim 1.This turbosupercharger can be utilized a woodruff key on the one hand, and the support (Cartridge) that assurance changes turbine geometry is axially fixed near this turbine wheel, on the other hand, can utilize heat shield plate to improve the thermal insulation of this bearing housing.
This purpose can be reached by the characteristics of claim 1.
The woodruff key of turbosupercharger of the present invention is formed by at least two material layers (but also can more than 2), and has the function that produces biasing force and improve function of shielding by increasing thermal resistance.Therefore, can be under high exhaust gas temperature assurance function.
In addition, if desired, can save the liquid-type cooling of bearing housing.
Subclaim requires to relate to the development of optimum of the present invention.
Owing to prepare several material layers, therefore can between material layer, form an air gap, with further biasing force and/or the thermal insulating properties improved.
Best, a material layer is made the form of pot, and another material layer is made flat disk.
This material layer can make the part of an integral body, perhaps also can make two divided portion.These two separate sections are under installment state, and one is placed on above another.
In addition, can constitute this material layer or also can select different materials by identical materials in principle.
In claim 11,, this woodruff key is defined as the object that to buy and sell independently for turbosupercharger of the present invention.
The accompanying drawing summary
Other details of the present invention, advantage and characteristics are from reference to the accompanying drawings to will be clear the explanation of the present invention.Wherein:
Fig. 1 represents to have the part of the turbosupercharger of the present invention of woodruff key of the present invention;
Fig. 2 is first embodiment's of expression woodruff key of the present invention sectional view; With
Fig. 3 for expression according to second embodiment of woodruff key of the present invention with Fig. 2 corresponding view.
The preferred embodiment explanation
Fig. 1 represents the part of turbosupercharger 1 of the present invention, because this diagram is enough to illustrate principle of the present invention.Certainly, this turbosupercharger 1 comprises all constitutional details that had usually, but as mentioned above, simple in order to represent, omit among Fig. 1.
Fig. 1 represents to be placed near the turbine shroud 2 of a turbine the bearing housing 3.Described bearing housing 3 be configured in this turbine shroud 2 and the compressor housing (not shown) of the compressor impeller that do not draw between.This bearing housing 3 comprises the bearing of axle.This bearing dot and dash line W with center line in Fig. 1 represents, because Fig. 1 only represents the top of turbosupercharger 1 of the present invention.
Turbine and compressor impeller are installed on axle W, and are bearing in this bearing housing 3 by corresponding bearing unit.
The woodruff key of being made by several layers of the present invention 4 is clamped between bearing housing 3 and the support K.This support K is made of the VTG disk 12 that has an axial stop 14 and a supporting blades annulus 15, and can move in this turbine shroud 2 vertically.In this example, be provided with two layers 5 and 6.Below, illustrate in greater detail these with reference to Fig. 2 and Fig. 3.
Fig. 1 is illustrated in the structure of the woodruff key 4 between this turbine shroud 2 and this bearing housing 3.Because the ledge structure of woodruff key 4 can obtain two supporting portions 10,11.As the expression at length of Fig. 1 institute like that, this woodruff key utilizes these two supporting portions to be bearing in the support of this turbine shroud 2 and turbine geometry variation respectively, on the corresponding part of this bearing housing 3.
Fig. 2 represents first embodiment of woodruff key 4 of the present invention.In this embodiment, these two material layers 5 and 6 are connected to each other as a part, form a uniform part.The material layer 5 that Fig. 2 represents to apply axial dipole field power have have around the pot shape structure of flange 13.In addition, this material layer 5 comprises a central recess 9, with the central recess 8 of this material layer 6 on same axis.Material layer 6 can be used as the heat shield plate of this material layer 5, but diameter dimension is identical or increase.Between this material layer 5 and 6, be provided with a further air gap 7 that improves insulating characteristics.
Fig. 3 represents another embodiment of this woodruff key.In the figure, this key is done as a whole with label 4 ' represent.Every other corresponding part is represented with label identical among Fig. 2.
Opposite with embodiment shown in Figure 2, the material layer 5 here and 6 is separately part, is expressed as installment state in Fig. 3, and promptly part is superimposed upon the position on another part.Except this class, can be with reference to the explanation of figure 2.
Can find out that from comprehensive study Fig. 2 and Fig. 3 under two kinds of situations, this material layer 6 is a flat disk.
            The label list
1 turbocharger/discharging turbocharger
2 turbine shrouds
3 bear boxes
4,4 ' woodruff key
(the woodruff key layer that 5-is used to be offset, 6-does not contact with bearing housing 5,6 material layers
The thermal-protective coating of layer 5)
7 air gaps
8,9 central recess
10,11 contact segments
12 VTG disks
13 around flange
14 axial stops
15 supporting blades annulus
16 the centers of support K on turbine shroud 2
The W axle
The support that the K turbine geometry changes

Claims (11)

1. a turbosupercharger (1) comprising:
The turbine shroud of a turbine wheel (2);
One is set at the support (K) that is suitable for the turbine geometry variation in the turbine shroud (2);
A bearing housing (3) is set between the compressor housing of turbine shroud (2) and compressor impeller, and the bearing unit of the axle (W) of this turbine wheel of supporting and this compressor impeller is set therein; With
A woodruff key (4,4 ') is set between this support (K) and this bearing housing (3), and is made of at least two material layers (5,6), and wherein, a material layer (6) is as the thermal-protective coating of another material layer (5) that constitutes a woodruff key layer;
It is characterized by, this woodruff key layer (5) be shaped on one around flange (13) and
This thermal-protective coating (6) makes a disk, and this woodruff key layer (5) at the rising edge (13) around this has is placed under installment state on this disk.
2. turbosupercharger as claimed in claim 1 is characterized by, and an air gap (7) is set between this material layer (5,6).
3. turbosupercharger as claimed in claim 1 or 2 is characterized by, and a material layer (5) is used as the form of pot.
4. as any described turbosupercharger in the claim 1~3, it is characterized by, another material layer (6) is made to a flat disk.
5. as any described turbosupercharger in the claim 1~4, it is characterized by, this material layer (5) is fixed on this support (K) in this turbine shroud (2) vertically.
6. as any described turbosupercharger in the claim 1~5, it is characterized by, this material layer (5,6) is interconnected into integral body.
7. as any described turbosupercharger in the claim 1~6, it is characterized by, this material layer (5,6) is part separately.
8. as any described turbosupercharger in the claim 1~7, it is characterized by, this material layer (5,6) is made of identical materials.
9. as any described turbosupercharger in the claim 1~7, it is characterized by, this material layer (5,6) is made of different materials.
10. as any described turbosupercharger in the claim 1~8, it is characterized by, this material layer (6) provides insulated heat for material layer (5).
11. a woodruff key (4,4 ') of the described turbosupercharger of preface as claimed in claim 1 (1) is characterized by, and has at least one feature in the feature of claim 1~10.
CN2005101317221A 2004-12-14 2005-12-13 Turbocharger Active CN1807847B (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP04029586.7 2004-12-14
EP04029586A EP1672177B1 (en) 2004-12-14 2004-12-14 Turbocharger

Publications (2)

Publication Number Publication Date
CN1807847A true CN1807847A (en) 2006-07-26
CN1807847B CN1807847B (en) 2011-10-05

Family

ID=34927770

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2005101317221A Active CN1807847B (en) 2004-12-14 2005-12-13 Turbocharger

Country Status (5)

Country Link
US (1) US7600969B2 (en)
EP (1) EP1672177B1 (en)
JP (1) JP4851178B2 (en)
KR (1) KR101149083B1 (en)
CN (1) CN1807847B (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102395770A (en) * 2009-04-20 2012-03-28 博格华纳公司 Anti-rotation method for a rolling element bearing cartridge
CN104975949A (en) * 2014-04-01 2015-10-14 博世马勒涡轮***有限两合公司 Exhaust gas turbocharger
CN108699958A (en) * 2016-03-07 2018-10-23 三菱重工发动机和增压器株式会社 Turbocharger
CN112576365A (en) * 2020-11-18 2021-03-30 潍柴动力股份有限公司 Engine and control method thereof

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US8545172B2 (en) * 2009-06-15 2013-10-01 Honeywell International, Inc. Turbocharger having nozzle ring locating pin and an integrated locator and heat shield
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US9752536B2 (en) 2015-03-09 2017-09-05 Caterpillar Inc. Turbocharger and method
US9739238B2 (en) 2015-03-09 2017-08-22 Caterpillar Inc. Turbocharger and method
US9650913B2 (en) 2015-03-09 2017-05-16 Caterpillar Inc. Turbocharger turbine containment structure
US10066639B2 (en) 2015-03-09 2018-09-04 Caterpillar Inc. Compressor assembly having a vaneless space
US9822700B2 (en) 2015-03-09 2017-11-21 Caterpillar Inc. Turbocharger with oil containment arrangement
US20180252160A1 (en) * 2015-08-28 2018-09-06 Borgwarner Inc. Turbocharger with insulation device
KR20190067850A (en) * 2016-11-02 2019-06-17 보르그워너 인코퍼레이티드 Turbines with multi-part turbine housings
US20190136712A1 (en) * 2017-11-03 2019-05-09 Borgwarner Inc. Multilayer Encapsulated Heat Shield for a Turbocharger
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Publication number Priority date Publication date Assignee Title
CN102395770A (en) * 2009-04-20 2012-03-28 博格华纳公司 Anti-rotation method for a rolling element bearing cartridge
CN104975949A (en) * 2014-04-01 2015-10-14 博世马勒涡轮***有限两合公司 Exhaust gas turbocharger
CN108699958A (en) * 2016-03-07 2018-10-23 三菱重工发动机和增压器株式会社 Turbocharger
CN108699958B (en) * 2016-03-07 2020-08-18 三菱重工发动机和增压器株式会社 Turbocharger
CN112576365A (en) * 2020-11-18 2021-03-30 潍柴动力股份有限公司 Engine and control method thereof

Also Published As

Publication number Publication date
JP2006170200A (en) 2006-06-29
US7600969B2 (en) 2009-10-13
JP4851178B2 (en) 2012-01-11
KR101149083B1 (en) 2012-05-25
EP1672177A1 (en) 2006-06-21
CN1807847B (en) 2011-10-05
EP1672177B1 (en) 2011-11-23
KR20060067864A (en) 2006-06-20
US20060127244A1 (en) 2006-06-15

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